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Implementation of Active Flow Control using Microjets on an RC Aircraft

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Implementation of Active Flow Control using Microjets on an RC Aircraft Dan Drake Phil Kreth Hussein Nabulsi Matt Tubtim Faculty Advisor: Dr. Farrukh Alvi – PowerPoint PPT presentation

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Title: Implementation of Active Flow Control using Microjets on an RC Aircraft


1
Implementation of Active Flow Control using
Microjets on an RC Aircraft
  • Dan Drake
  • Phil Kreth
  • Hussein Nabulsi
  • Matt Tubtim
  • Faculty Advisor Dr. Farrukh Alvi
  • Sponsor Dr. Gregg Abate (Eglin AFB)

2
Background
  • Flow Separation

Flow separated 16 AOA
Reattached flow 5 psig _at_ microjets
04.03.2008
3
Motivation
  • ONERA D Airfoil
  • Span 1 m, Chord 0.35
  • U? 45 m/s, ? 14?
  • Control applied to 40 of span

Baseline flow
Flow with Control
Conducted at the Université de Poitiers, France
Images Video Courtesy of Dr. Farrukh Alvi
04.03.2008
4
Motivation
20-30 gain in CL Control applied to 40 of span
Images Courtesy of Dr. Farrukh Alvi
04.03.2008
5
Needs Assessment
  • Implement microjets on RC Airplane
  • Remotely activate each wing
  • Run time should be 30 secs or more
  • Delay stall and improve lift
  • Use off-the-shelf items only
  • Budget 1,50000

04.03.2008
6
Wind Tunnel Testing
  • Paint Testing
  • Uncertainty in interpretation
  • Smoke Wire
  • Minimum WT speed too high
  • Tuft Testing
  • Success

04.03.2008
7
Flow Reattachment Video
04.03.2008
8
Air Supply Method
9
Air Supply Method
10
Performance Measurements
11
Final Design Schematic
04.03.2008
12
Actual Design
04.03.2008
13
Final Design Components
Overhead View
Close-up view Tank Regulator Valves
04.03.2008
14
High Pressure Tank Location
04.03.2008
15
Shielding for High Pressure Cylinder
04.03.2008
16
Pressure Manifolds and Microjets in Wing
to microjets
from valves
04.03.2008
17
Budget Weight
  • Added Weight 10 lbs
  • Total Weight 14 lbs

04.03.2008
18
Test Plan
  • Video aircraft on ground
  • Show all systems in working order
  • Flight testing, no control
  • Flight testing, with control
  • Acquire video from on-board camera

04.03.2008
19
Flight Test Goals
  • Dont crash!
  • Demonstrate reattachment

04.03.2008
20
Flight Test Video
04.03.2008
21
Outcomes Conclusions
  • System was successful
  • No bad landings
  • Microjets remotely activated
  • Reattached flow demonstrated
  • Proposed Future Work
  • Demonstrate Roll Control
  • Measure CL and CD improvements

04.03.2008
22
Special Thanks
  • Eglin Air Force Base
  • Dr. Gregg Abate
  • AAPL FAMU-FSU
  • Dr. Farrukh Alvi
  • Mechanical Engineering Dept
  • Dr. Cesar Luongo
  • Mr. Jon Cloos

04.03.2008
23
Questions and Comments
04.03.2008
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